High reliability memory module with a fault tolerant address and command bus

ABSTRACT

A high reliability dual inline memory module with a fault tolerant address and command bus for use in a server. The memory module is a card approximately 151.35 mm or 5.97 inches long provided with about a plurality of contacts of which some are redundant, a plurality of DRAMs, a phase lock loop, a 2 or 32K bit serial EE PROM and a 28 bit and a 1 to 2 register having error correction code (ECC), parity checking, a multi-byte fault reporting circuitry for reading via an independent bus, and real time error lines for determining and reporting both correctable errors and uncorrectable error conditions coupled to the server&#39;s memory interface chip and memory controller or processor such that the memory controller sends address and command information to the register via address/command lines together with check bits for error correction purposes to the ECC/Parity register. By providing the module with a fault tolerant address and command bus fault-tolerance and self-healing aspects necessary for autonomic computing systems compatible with industry-standards is realized. The memory module corrects single bit errors on the command or address bus and permits continuous memory operation independent of the existence of these errors and can determine any double bit error condition. The redundant contacts on the module prevents what would otherwise be single points of failure.

CROSS-REFERENCE TO RELATED APPLICATIONS

This application is a divisional application of U.S. patent application Ser. No. 10/413,605, filed Apr. 14, 2003 now U.S. Pat. No. 7,234,099, the contents of which are incorporated by reference herein in their entirety.

FIELD OF THE INVENTION

This invention relates generally a high-reliability memory module with a fault tolerant address and command bus for use as a main memory that will achieve the degree of fault-tolerance and self-healing necessary for autonomic computing systems.

BACKGROUND OF THE INVENTION

Memory modules are well known to the prior art and have been and are presently being used in practical applications such as in computers and other equipment using solid state memories.

Broadly speaking, currently available main memories offer bandwidths in the range of 1.6 to 2.6 GB/s, and although some memories provide for limited data path error correction most offer no means of any error correction. Furthermore, memory modules for server products usually include redrive logic for address and command inputs, and clock re-synchronization and redrive circuitry to ensure accurate clock timings at each device on the memory assembly. Although these solutions provide systems with the ability to achieve the specified bandwidth objectives, the overall quantity and types of failures in the memory subsystem, outside the data path itself, has actually increased due to the added circuitry associated with each memory device. Simultaneously, as servers are more widely utilized in business, many server applications simply cannot accept periodic unplanned system outages caused by failed memory modules. Thus the emphasis and need of improved overall system reliability is increasing dramatically and requires a comprehensive system solution that includes both a high degree of fault tolerance and overall reliability.

The present invention provides such a comprehensive system solution that includes the high degree of fault tolerance and the overall differentiated system reliability long desired in the server market.

Other possible solutions, such as memory mirroring, symbol slicing and extensive forms of fault rejection and redundancy, provide enhanced memory subsystem reliability, but, due to negative impacts such as increased cost, power, and reduced performance, have been considered only for niche applications where price is not of high importance as these subsystem quality enhancements are very expensive to implement. Therefore solutions suitable for the low or midrange server markets have not been available.

Consequently the industry has long sought a simple, relatively inexpensive and reliable solution that provides differentiated product quality, that provides an adequate level of asset-protection that does not endanger the reliability of the system through the use of reduced-function memory assemblies and yet is cost competitive.

SUMMARY OF THE PRESENT INVENTION

The present invention is directed to a high reliability memory controller/interface module, provided with a high degree of compatibility with industry-standard solutions, capable of meeting the desired performance and reliability requirements and interfacing with the presently available memory modules, as well as with existing or enhanced support devices. The present invention accomplishes all these ends, resulting in an enhanced reliability memory solution at low cost.

An object of the present invention is a 28 bit 1:2 register, intended for use with Dual Inline Memory Modules (DIMMs) having Dynamic Random Access Memory chips thereon. The register of the present invention has added thereto error correction code (ECC) logic to correct single bit errors on the command or address bus, and permit continuous memory operation independent of the existence of these errors.

Another object of the present invention is to include in such DIMMs error latches and an error reporting mode whereby the system may interrogate the device to determine the error condition thereby allowing accurate fault determination and preventive maintenance—thereby reducing unplanned system outages.

A further object of the present invention is to include redundant contacts on all connectors/DIMM interconnects that would otherwise be considered single points of failure whereby an intermittent or permanent contact failure would result in an unplanned system outage.

Still another object of the present invention is to provide the DIMM with key operational features such as chip select gating of key inputs and programmable delay for un-gated inputs, thereby reducing module power and offering increased operational flexibility.

A further object of the invention is to provide a DIMM that can be readily utilized in presently available controllers in a manner most applicable to the market needs.

Another further object of the present invention is to have a DIMM that uses connectors similar to those presently in use so that prior art contacts, molds, handlers and related production tools can continue to be used such that the modules can be more cheaply produced with additional density while providing value-added reliability, and other value-add attributes, such as a higher memory packaging density with minimal additional production costs.

The DIMM of the present invention is comprised of a printed circuit board having a front side and a back side and a plurality of dynamic random access memories (DRAMs) or synchronous dynamic random access memories (SDRAMs) affixed to both the front surface and the back surface. On a first edge of the front surface of said board there is provided one hundred and thirty eight (138) contacts for connecting circuitry, external to the card, to the SDRAMS and related devices on the DIMM and on the same first edge on the rear side of the card there is provided an additional one hundred and thirty eight (138) external circuitry connecting contacts so that the board has a total of two hundred and seventy six (276) external circuitry connecting contacts thereon. The contact means provided on the front and the back sides of the printed circuit card provide for electrically connecting the external circuitry to the SDRAMs in a direct or indirect manner.

Still another further object of the present invention is to provide a server memory structure having a dual inline memory module or DIMM provided with selective redundant contacts, a phase lock loop, 2 or 32K bit serial electronically erasable programmable read only memory (EE PROM) and a 28 bit, 1 to 2 register having error correction code (ECC), parity checking, a multi-byte fault reporting register, read via an independent bus, and real time error lines for both correctable errors and uncorrectable error conditions. More particularly the server of the present invention comprises a novel DIMM provided with a new and unique ECC/Parity Register coupled to the memory interface chip 18 which is in turn coupled to the Memory controller or processor 19 such that the memory controller sends address and command information to the register via address/command lines together with check bits for error correction purposes to the ECC/Parity register.

Still another object of the invention is to provide for detecting if the module installed in the server can monitor the address and control bus integrity, correct errors on the address and control bus, report errors and log and counts errors.

Still an other object of the invention is to provide for Parity error reporting in which the parity signal is delivered one cycle after the address and command to which it applies, and the error line be driven low two clocks after the address and command bits are driven to the DRAMs from the register on the DIMM. After holding the error line low for only 2 clock cycles, the driver can be disabled and the output permitted to return to an undriven state (high impedance) thus allowing this line to be shared by multiple modules.

Still further the invention provides means for and a method for adjusting the propagation delay, for signals on the memory module that are not included in the ECC circuitry, such that the signals can be selectively re-driven within one or two clock cycles.

Still further the present invention permits operation of the memory module in parity mode, such that unused ECC check bit inputs are held at a low level thus ensuring that these inputs are at a known and quiescent state.

Still further the present invention provides for reducing the probability of Single Point of Failures occurring by providing selected signals with redundant contacts directly on the opposite side of the DIMM from the original function contact thereby reducing the probability of a contact failure resulting in an unplanned system outage.

Even further the present invention provides for operating a module of the present invention consistent with conventional non-ECC protected modules, by removing the secondary registers (post-ECC) from the delay path by setting the /ECC Mode control pin to a high level.

These objects, features and advantages of the present invention will be become further apparent to those skilled in the art from the following detailed description taken in conjunction with the accompanying drawings wherein:

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is a block diagram of a typical server memory arrangement.

FIG. 2 is a block diagram of the enhanced server memory arrangement of the present invention;

FIGS. 3A and 3B are plan views respectively of the front and back of the two hundred and seventy six (276) pin dual inline memory module (DIMM) of the present invention;

FIGS. 4A and 4B are schematic views of the ECC/Parity register, shown in FIG. 3A;

FIG. 5 is a block diagram of the single error correction/double error detection error correction code (SEC/DED ECC) circuit of FIG. 4B;

FIG. 6 describes, in H-matrix form, the preferred ECC code selected for the module of FIG. 3;

FIGS. 7A, 7B and 7C show the designated contacts or pin connections for the DIMM of FIGS. 3A and 3B; and

FIG. 8 shows the timing diagram used with the present invention.

DESCRIPTION OF THE PREFERRED EMBODIMENT

A full appreciation of the features and advantages of the present invention can best be gained by reference to the drawings and more particularly to the figures where: FIG. 1 is a block diagram of a typical server memory arrangement; FIG. 2 is a block diagram of the enhanced server memory arrangement of the present invention; FIGS. 3A and 3B are plan views respectively of the front and back of the 276 contact dual inline memory module (DIMM) of the present invention; FIGS. 4A and 4B are schematic views of the register, parity and error correction circuits shown in FIGS. 3A and 3B; FIG. 5 is a block diagram of the single error correction/double error detection error correction code (SEC/DED ECC) circuit of FIG. 4B; FIG. 6 describes, in H-matrix, form the preferred ECC code selected for the module of FIG. 3A; FIGS. 7A, 7B and 7C show the designated pin connections for the DIMM of FIGS. 3A and 3B and FIG. 8 shows the timing diagram used with the present invention.

In FIG. 1 there is illustrated, in schematic form, a block diagram of a typical server memory arrangement as might be found in any currently available server which can employ a plurality of dual inline memory modules (DIMMs). It should be understood that many such DIMMs would be used in actual practice but for ease of illustration only one prior art DIMM 10 is shown in FIG. 1. DIMM 10, is a printed circuit card on which there is provided a plurality of either synchronous dynamic random access memories or dynamic random access memories circuits 11, herein after collectively referred to as DRAM. Each DRAM 11 on the DIMM 10 has a plurality of output pins that are coupled, via the printed circuitry on the DIMM to the contacts on the DIMM and theses contacts are further coupled, via a data line 15, to a memory interface chip 18 and to a memory controller or processor 19. Each DRAM on the DIMM is further, coupled via such DIMM contacts, to a register 12 and to a phase locked loop circuit 14 on the DIMM. The phase locked loop 14 (PLL) is connected via clock line 17 to the memory interface chip 18. The register 12 is also coupled to the memory interface chip 18 via an address and command (cmd) bus 16. The memory interface chip 18 is coupled to the memory controller 19 via the data line 15, address and command line 16 and Clock line 17. It should be understood that although only one such DIMM is shown in this figure that in actuality the server would contain many such DIMMs. Such other DIMMs would be coupled in a like manner to the memory interface chip 18 and memory controller 19 via data, address and command lines. Since such servers and their operation are so well known to those skilled in the art, further description of such servers and their operation is not deemed necessary.

Turning now to FIGS. 2, 3A, 3B, 4A, 4B, 5 and 8 the enhanced server memory arrangement of the present invention will be described.

In FIG. 2 there is illustrated, in schematic form, a block diagram of a server memory arrangement employing the present invention. In this FIG. 2 the server comprises a novel DIMM 20 provided with a novel ECC/Parity Register chip 21 coupled to the memory interface chip 18 which is in turn coupled to the memory controller or processor 19. It should be understood that the chip 21 need not include both the ECC function and the parity function. For example, the chip 21 could have just the ECC function alone or just the parity function alone and still operate in accordance with the present invention. More specifically, as shown in this FIG. 2, the memory interface chip 18 sends and receives data from the DIMMs via the data line 15 and sends address and commands via line 16. The memory interface chip 18 then sends and receives data, via line 15, to the DRAMs and sends address and command information to the register chip 21 via add/cmd line 16 and check bits for error correction purposes to the ECC/Parity register chip 21 via line 25.

FIGS. 3A and 3B show respectively the front and back views of the novel DIMM 20 of the present invention. Generally speaking DIMMs are printed circuit cards designed to carry a plurality of DRAMs 22 thereon and the DRAM output pins (not shown) are connected via the printed circuit to selected connectors 23 along the edge of both the back and front sides of the card and are often provided with a single indexing key or notch 9 on the connector edge. The use and manufacture of such DIMMs is well known and need not be further described herein. The DIMM of the present invention however is novel and is designed to address several of the most significant contributors to unplanned and often catastrophic system outages encountered in the prior art DIMMs. The improvements in the DIMM of the present invention are realized especially by enlarging the length of DIMM 20 to between 149 mm and 153 mm. Nominally the DIMM 20 is 151.35 mm (5.97 inches) long and its width is 30.48 mm (1.2 inches). The width of the DIMM is not critical and the DIMM need only be wide enough to accommodate the DRAMs installed thereon. The length of the DIMM however must be such that the DIMM 20 can accommodate additional signal contacts, up to 138, as well as up to thirty-six DRAMs 26 having a body size up to 14 mm by 21 mm and have a locating key or notch 9 a distance of between 82.675 mm from one end of the DIMM and 68.675 mm from the other end of the DIMM as shown. Again it should be understood that these dimensions are nominal and may vary plus or minus 3 mm in various implementations. The DIMM can also be provided with additional notches 9 a and 9 b on each side, i.e., the shorter edges of the DIMM 20. These dimensions permit the DIMM, of the invention, to accommodate placing up to eighteen DRAMs on the front surface and up to an additional eighteen such DRAMs on the rear surface. Further, as shown in FIG. 3A, on the front of each DIMM 20, in addition to the DRAMs, there is positioned a phase locked loop chip 24 and the novel ECC/Parity Register chip 21 of the present invention. This novel ECC/Parity Register chip 21 will be further described below and in detail in conjunction with FIGS. 4A and 4B It should be understood that the phase locked loop chip can be eliminated if its circuitry is provided on the register chip 21.

This new, improved, larger sized DIMM 20, shown in these FIGS. 3A and 3B, also achieves a further significant improvement in the interconnect failure rate for the larger size of the module permits the connector system to accommodate two hundred and seventy-six contacts or pins 23. These pins are numbered and coupled to respective inputs as shown in FIGS. 7 a, 7 b, and 7 c. Contact or pin number one (1) is identified and shown in FIG. 3A as contact 23A and is on the left hand side of the front side of the DIMM 20 and is positioned approximately 5.175 mm from the left edge of the DIMM and 77.5 mm from the center of the notch 9. Contact or pin number one hundred and thirty-eight (138) is identified and shown in FIG. 3A as contact 23B and is on the right hand side of the front side of the DIMM 20 and is positioned approximately 5.175 mm from the right edge of the DIMM 20 and approximately 63.5 mm from the center of the notch 9. Contact or pin number one hundred and thirty-nine (139) is identified and shown in FIG. 3B as contact 23C and is directly opposite contact number one 23A and is also positioned approximately 5.175 mm from the left edge of the DIMM 20 and is also 77.5 mm from the center of the notch 9. Contact or pin number two hundred and seventy-six (276) is identified in shown in FIG. 3B as contact 23D and is directly opposite contact number one hundred and thirty-eight 23B and is also positioned approximately 5.175 mm from the right edge of the DIMM 20 and 63.5 mm from the center of the notch 9. The greater size of this DIMM 20 also accommodates the inclusion the new and a larger ECC/Parity register 21 required by the present invention. Because the two hundred and seventy-six contacts or pins 23 on this larger DIMM are more than sufficient to meet the needs of all the circuitry on the DIMM this means that the DIMM provides extra or redundant contacts. These extra or redundant contacts or pins 23 can now be used to provide additional protection for certain selected signal or voltage lines, for which error correction is not possible. The present invention by providing such redundant contacts effectively eliminates concerns such as contact failures on clock inputs, CS, CKE, and ODT inputs, Vref inputs, and other signals not protected by ECC. Other benefits include the elimination or reduction of concerns regarding power supply noise and/or voltage drops due to scarcity of voltage (VDD) contacts in the data region as well providing additional ground pins in the address/control region on the DIMM 20. The larger contact count of the present invention also permits the DIMM 20 to be wired such that they are consistent with prior art DIMMs. The additional contacts 23 also permit the inclusion of ECC check bits, associated with address and command inputs, allowing for real-time system monitoring of faults associated with these inputs, as well as system interrogation of fault counts and attributes. These faults would result in catastrophic system outages in conventional prior art systems using the smaller prior art DIMMs.

It should be understood that although only one DIMM 21 is shown in the FIGS. 1 and 2 that, in actuality, the server would contain many such DIMMs. As noted above, the DIMM 21, of the present invention, is provided with a plurality of SDRAMs 22, a phase locked loop circuit 24 and the ECC/Parity register 21. The ECC/Parity register 21 on DIMM 20 includes unique error correction code (ECC) circuitry that is coupled to the memory interface chip 18 via line 25 to provide even greater significant reliability enhancement to such servers. The inclusion of this new, improved error correction code (ECC) circuitry results in a significant reduction in interconnect failure.

FIGS. 4A and 4B together comprise a schematic view of the novel ECC/Parity register 21 on DIMM 20 where, for clarity in description, it is shown as comprised of two distinct sections 21 a and 21 b. FIG. 4A shows the enhanced function 28 bit 1:2 register segment 21 a of the present invention and FIG. 4B shows the error correction code circuit segment 21 b. The error correction code circuit ECC segment 21 b, shown in FIG. 4B, corrects for single bit errors and thus permits continuous memory operation independent of the existence of these errors. This ECC segment also includes a parity operating mode circuitry together and error reporting circuitry. The novel ECC/Parity register 21 on DIMM 20 thus provides leading-edge performance and reliability and key operational features different from and unavailable from the prior art while retaining timing requirements generally consistent with the JEDEC 14 bit 1:2 DDR II register.

More particularly, the register segment 21 a contains a plurality of so called differential bit receivers 40 a through, 40 e, 41, 42 a through 42 n, 43, 44, 45 a, 45 b, 46 a and 46 b and a single amplifier 47. Each of these differential receivers 40 a through 40 e, 41, 42 a through 42 n, 43, 44, 45 a, 45 b, 46 a and 46 b has two inputs and a single output. One of the inputs of each differential receiver 40 a through, 40 e, 41, 42 a through 42 n, 43, 44, 45 a, 45 b, 46 a and 46 b is coupled to a reference voltage source 28. The second input of the each of the differential receivers 40 a through, 40 e, 41, 42 a through 42 n, 43, 44, 45 a, 45 b, 46 a and 46 b are coupled to respective inputs 30 a through, 30 e, 31, 32 a through 32 n, 33 a, 33 b, 34, 35 a, 35 b, 36 a and 36 b.

Receiver set 40 a through 40 e is comprised of five receivers of which only the first and the last receivers 40 a and 40 e are shown. Receivers 40 a through 40 e have their second inputs respectively coupled to respective check bit lines 30 a through 30 e and their outputs connected through respective primary multiplexers 60 a through 60 e to the inputs of respective primary latches 70 a through 70 e. Typically the check bit lines are contained in a bus that contains a set of five such check bit lines. However, for simplification of the drawing and ease of description only, FIG. 4 a shows only the first and the last check bit lines 30 a and 30 e of the set and the first and last of the receivers 40 a through 40 e. It being understood that each receiver in the set 40 a through 40 e has one of its respective inputs coupled to a respective one of a set of check bit input lines 30 a through 30 e and its output to a respective one of a set of three input multiplexers and thence to a respective one of a set of three input primary latches.

The second input of the differential receiver 41 is coupled to a check bit 0/Parity_in signal line 30.

Receiver set 42 a through 42 n is comprised of twenty two receivers coupled to a data line bus typically containing twenty two data lines 32 a through 32 n. However, for simplification of the drawing and ease of description only, FIG. 4 a shows only the first and the last data lines 32 a and 32 n of the set and the first and last of the receivers 42 a through 42 n are shown in the drawing. The first receiver 42 a is shown as having its first input coupled to data bit line 32 a and its output coupled to the first input of multiplexer 62 a whose output is coupled to a first input of primary latch 72 a and the last receiver 42 n is shown as having its first input coupled to data bit line 32 n and its output coupled to the first input of multiplexer 62 n whose output is coupled to a first input of primary latch 72 n. Each respective receiver in set 42 a through 42 n has an input coupled to a respective one of data lines in set 32 a through 32 n and their outputs connected through respective primary multiplexers 42 a through 42 n to the inputs of respective primary latches 62 a through 62 n. All the primary multiplexers and latches in the set 42 a through 42 n are identical to those shown connected to receivers 42 a and 42 n. Thus each receiver in the set has one of its respective inputs coupled to a respective one of a set of data bit input lines and its output to a respective one of a set of two input multiplexers and thence to a respective one of a set of primary latches. These signals are inputted from the memory interface chip 18 in FIG. 2 and are re-driven only when one or more of the inputs 33 a, 33 b, or 34 are low.

As previously noted, the second input of the differential receiver 41 is coupled to a check bit 0/Parity_in signal line 30. The output of the differential receiver 41 is coupled to an input of multiplexer 61 whose output is coupled to a primary latch 71. The check bit 0/Parity_in signal is interpreted as an ECC check bit from the memory controller or as a parity bit depending on the setting of ECC mode input 136 (FIG. 4B) Clock inputs 131 are fed to all the primary latches 70 a through 70 e, 71, 72 a through 72 n, 73, 74, 75 a, 75 b, 76 a and 76 b. The Check bits 1-5 at inputs 30 a through 30 e are in a dont care state when the register is being operated in parity mode and will be held low. When these inputs are operated in parity mode, a parity in signal will be provided on the Check bit 0/Parity_in signal line 30 and maintain odd parity across the data inputs 32 a through 32 n, at the rising edge of the clock signal (CK) at input 131 that immediately follows the rising edge of clock 131 that occurred simultaneously with the associated data inputs 32 a through 32 n.

The second inputs of the differential receivers 43 and 44 are respectively coupled to chip select lines /CS0 and /CS1 and the outputs of the differential receivers 43 and 44 are coupled respectively to the first inputs of primary latches 73 and 74 as well as to the first and second inputs of a three input select NAND gate 63. The output of NAND gate 63 is coupled to the selection input of the multiplexers 60 a through 60 e, 61 and 62 a through 62 n. These lines initiate DRAM address/command decodes and as such at least one will be low when a valid address/command signal is present and the register can be programmed to redrive all the data inputs when at least one chip select input (CS0,/CS1) 33 a, 33 b is low. The third input of this NAND gate 63 is coupled to CS gate enable circuit 34 which can be set low to cause multiplexers 60 a through 60 e to pass signals from receivers 32 a through 32 n independent of the levels on inputs 33 a and 33 b.

The output of differential receiver 43 and 44 are also respectively coupled through the lines 172 and 174 and the AND gate 175 (FIG. 4B) whose output is coupled to the error logic circuit 100 also shown in FIG. 4 b.

Receiver 45 a has an input coupled to the clock enable signal source 35 a (CKE0) and an output coupled to the primary latch 75 a.

Receiver 45 b has an input coupled to the clock enable signal sources 35 b (CKE1) and an output coupled to the primary latch 75 b.

Receiver 46 a has an input coupled to the on die termination line signal input line 36 a (ODT0) and an output coupled to the primary latch 76 a.

Receiver 46 b has an input coupled to the on die termination line signal line 36 b (ODT1) and an output coupled to the primary latch 76 b.

Receiver 47 has an input coupled to the reset (/RST) signal line 37. The inputs 35 a and 35 b (CKE0, CKE1) 36 a and 36 ba (ODT0, ODT1) are provided from the memory interface chip 18 and are not associated with the Chip Select (CS) inputs 33 a and 33 b, and signal from source 37 (/RST) driving amplifier 47 is an asynchronous reset input and, when low, resets all the primary latches 70 a through 70 e, 71, 72 a through 72 n, 73, 74, 75 a, 75 b, 76 a, 76 b and all the secondary latches 92 a through 92 n, 93, 94, 95 a, 95 b, 96 a and 96 b thereby forcing the outputs low. This signal from source 37 (/RST) also resets the error bus registers and error lines from the error logic circuit 100.

Coupled to the above described register of FIG. 4A is the unique error correction code circuit arrangement of FIG. 4B.

In FIG. 4B, module location identification is provided to error logic circuit 100 which is more fully described in conjunction with FIG. 6 below. This module location identification is provided to error logic circuit 100 through receivers 79 a,79 b, and 79 c whose inputs are coupled to DIMM address input range sources (SA0, SA1, SA2) 78 a, 78 b and 78 c and whose outputs are coupled to an error logic circuit 100. The signals from sources (SA0, SA1, SA2) 78 a, 78 b and 78 c define the DIMM address which is then reported on the error bus when requested by the system. This error logic circuit 100 is controlled by a signal from the NAND gate 175 when either of the DRAM chip select signal sources (/CS0) 33 a and (/CS1) 33 b are active. The error logic circuit 100 further has a reset signal source 180 coupled thereto.

Also included in the error correction code circuit of FIG. 4 b is a SEC/DED ECC circuit 90 which is more fully described in conjunction with FIG. 5 below. Coupled to this SEC/DED ECC circuit are the outputs of primary latches 70 a through 70 e, 71 and 72 a through 72 n. This SEC/DED ECC circuit 90 provides three outputs 109, 110, and 111 to the error logic circuit 100. These outputs are: a correctable error (CE) line 109, an uncorrectable error (UE) line 110 and a parity error bit line 111 fed to the error logic circuit 100 which provides outputs regarding correctable and uncorrectable errors on output lines 120 and 121. When either error line (CE) 109 or uncorrectable error line (UE) 110 is low this indicates that an error was identified as being associated with the address and/or command inputs (either correctable or uncorrectable). The error lines 120,121 will be active, i.e., low, for two clock cycles simultaneous with the re-driven address/command data when operating in ECC mode or delayed by two clock cycles when operating in parity mode. The logic error circuit 100 also provides an Error Bus (Inter Integrated circuit or IIC) 122 for external collection of error information such as error type, DIMM address, error count and status of the 28 input and internally generated syndrome bits at the time of the first fail. The information remains latched until a reset command is written to bus 122 or /RST input 37 is switched low. The selected IIC protocol allows unique byte addressing of the nine registers, consistent with the present industry standard protocol for serial program decode electronic erasable programmable read only memory (SPD EEPROM) and is well known to the art.

This SEC/DED ECC circuit 90 also has data bit outputs coupled through secondary latches 92 a through 92 n to a first input of all the output or secondary multiplexers 102 a through 102 n. The output of register latches 72 a through 72 n labeled BYPASS are directly connected to the second input of the output or secondary multiplexers 102 a through 102 n thereby allowing the SEC/DED ECC circuit 90 to be bypassed depending on the ECC mode input 123.

The output of the primary or register latches 73, 74, 75 a, 75 b, 76 a and 76 b are all coupled to a first input of secondary or output latches 93, 94, 95 a, 95 b, 96 a and 96 b and through these secondary latches 93, 94, 95 a, 95 b, 96 a and 96 b to a first input of output or secondary multiplexers 103, 104, 105 a, 105 b, 106 a and 106 b. The outputs of primary latches 73, 74, 75 a, 75 b, 76 a and 76 b are connected directly to a second input of output or secondary multiplexers 103, 104, 105 a, 105 b, 106 a and 106 b thereby allowing secondary latches 93, 94, 95 a, 95 b, 96 a and 96 b to be bypassed based on the /Delay CKE input 124 and /ECC mode input 123.

A control circuit comprised of a differential register 130 that has a first input coupled to a CK signal input 131, a second input coupled to a /CK signal input 132 and its output coupled to a second input all the primary latches 70 a through 70 e, 71, 72 a through 72 n, 73, 74, 75 a, 75 b, 76 a and 76 b and to the second input of all the output or secondary latches 92 a through 92 n, 93, 94, 95 a, 95 b, 96 a and 96 b and to the error logic circuit 100 via line 88. The /ECC mode signal source 135 is coupled to a selection third input of secondary multiplexers 102 a through 102 n, 103 and 104 and to the error logic circuit 100. The output or secondary multiplexers 105 a, 105 b, 106 a and 106 b have their selection inputs coupled to a source 124 of /Delay, CKE_ODT signals.

The ECC code selected for this module is a single error correction/double error detection (SEC/DED) code and is shown in the H-Matrix depicted in FIG. 6. The use of this SEC/DED code ensures that all single errors associated with the address and control bits are detected and corrected and that all double bit errors are detected. It should be noted that interconnect failures almost exclusively begin as single point fails, with other failures possibly occurring over time dependent or independent of the root cause of the initial fail.

In summary the present invention describes unique DIMM having an enhanced 28 bit 1:2 register with added error correction code logic (ECC) incorporated therein for correcting single bit errors while permitting continuous memory operation independent of the existence of these errors. A parity operating mode is also provided, in conjunction with error reporting circuitry to permit the system to interrogate the device to determine the error condition.

The above described 28 bit 1:2 register of the present invention provides key operational features, which differ from existing register designs intended for memory module applications and includes: Error detection and correction on key inputs; programmable delay for un-gated inputs; parity mode; reset circuitry; error reporting and identification and reporting of the DIMM address.

CS gating of key inputs, e.g., /CS0 and /CS1, is provided as a means of reducing device power for the internal latches which will only be updated when one or both of the chip select CS) inputs are active low (and chip select gate enable tied high) at the rising edge of the system clock. The twenty two chip select-gated signals associated with this function include addresses continuously re-driven at the rising edge of every clock depending on the state of chip select. However, the chip select gating function can be disabled by tying the chip select gate enable input low thereby enabling all internal latches to be updated on every rising edge of clock.

Programmable delay for un-gated inputs (/Delay CKE-ODT) associated with CKE and ODT (DRAM signals), the inputs will be latched and re-driven on each rising edge of the clock signal (CLK,) independent of the state of the chip select (CS) signals. However, since some controllers may be designed with limited flexibility regarding latency for these signals vs chip select (CS), address (Addr), row address strobe (RAS), column address strobe (CAS) and write enable (WE), a delay block can be selected to re-align the timing relationships which are offset by 1 clock when the error correction code circuitry (ECC) is enabled.

ECC Mode (/ECC Mode low): For all inputs gated by CS, on-chip SEC/DED ECC logic is enabled and the signal received on CHK0/Parity in is received as check bit 0 when /ECC Mode input is low. This ECC logic will operate across 28 inputs (22 ‘CS-gated inputs and the 6 check bits) and will correct all single bit errors and detect all double bit errors present on the twenty two chip select gated data inputs. If a correctable error is detected, /Error (CE) will be driven low for two clocks and errors will be counted and latched in the error bus registers for the 28 inputs if this is the first error since a reset is issued. Any double bit error will also be detected (as well as many other errors that are not correctable), and will be reported on the /Error (UE) error line (driven low for two clocks) and in the error bus registers if this error is the first since a Reset is issued. Although CS0-1 are not included in the ECC logic, the propagation delay of the CS output signals will track the signals included in the ECC logic (1 additional clock of latency)

In addition to the above ECC mode, the same twenty two chip select gated data signals can be operated in ‘parity mode (/ECC Mode high), whereby the signal received on CHK0/Parity in line is received as parity to the register one clock pulse later than the chip select gated data inputs. The received parity bit is then compared to the parity calculated across these same inputs by the register parity logic to verify that the information has not been corrupted. The twenty two chip select gated data signals will be latched and re-driven on the first clock pulse and any error will be reported two clock pulses later via the uncorrectable /Error (UE) line (driven low for two clock pulses) and in the Error Bus Registers. No correction of errors will be completed in this mode. The convention of parity, in this application, is odd parity (odd numbers of 1s across data and parity inputs equals valid parity).

The /RST signal input is used to clear all internal latches (including the error registers), and all outputs will be driven low quickly except the error lines which will be driven high.

Error reporting circuitry is included to permit external monitoring of DIMM operation. Two open-drain outputs are available to permit multiple modules to share a common signal line for reporting an error that occurred during a valid command (/CS=low) cycle (consistent with the re-driven signals). These two outputs are driven low for two clocks to allow the memory controller time to sense the error./Error (CE) indicates that a correctable error occurred and was corrected by the ECC logic, /Error (UE) indicates that an uncorrectable error occurred and depending on the mode selected is an uncorrectable ECC error or a parity error. Note that the timing of /Error (UE) is different in parity mode vs ECC mode.

In addition, an error bus (9 registers that can be read and reset via an IIC bus) is available to permit the device to be interrogated for additional error information, such as the error type (correctable, uncorrectable or parity error), error count and the memory card location (via the SAO-2 address pins which are conventionally wired only to the separate serial program decode (SPD) electronic erasable programmable read only memory (EE PROM). Other information is also available for diagnostics such as the signals received by the register (address/command, control signals, check bits, parity bit) when a chip select (CS) is active low and the associated syndrome bits so that they can be decoded to determine which of the 28 input signals (22 ‘CS-gated plus 6 check bits) or internal ECC logic failed. These registers will contain information about the first fail, and the error counter will continue to increment until it is reset or reaches the full count (64K). All registers can be reset by writing the reset error bus command on the IIC bus, or via the /RST pin.

In addition to the use of the ECC structure defined above (included in both the memory interface chip and the register on the DIMM), redundant contacts are included on the module pinout to effectively eliminate other possible SPOF (single-point-of-failure) contributors in the interconnect system. Contacts that cannot be protected by the ECC structure described above, for various reasons, include the following: voltage reference (Vref), Clocks, Chip Selects (CS), CKEs, ODTs, VSS/VDD contacts or pins, Error lines, data input on the IIC bus (SDA), data clock on the IIC bus (SCL) and related signals. In the present invention each of these contacts is provided with a first contact on a first side of the DIMM and a redundant contact directly opposite the first contact on the opposite side of the DIMM. For example if the voltage reference source 28 is applied via contact or pin 1 on the front side of the DIMM it is also applied via contact or pin 139 on the back side of the DIMM with contact 1 being direct opposite contact 139. Similarly the SDA signal is applied via contact or pin 135 on the front side of the DIMM and also via the contact or pin 273 on the back side of the DIMM and the SCL signal is applied via contact or pin 136 on the front side of the DIMM and also via contact or pin 274 on the back side of the DIMM. A full description of the contact or pin assignment matrix for the present invention is shown in FIGS. 7A, 7B and 7C. The specific contact placement is selected to maximize fault tolerance. By providing such opposite redundant contacts, problems caused, for example, by a slight bowing of the DIMM will cause low contact pressure on a contact on one side of DIMM but high pressure on the opposing contact. In such cases good signal flow will always be assured when such redundant and opposing contacts, as discussed above, are used. These opposing and redundant contacts will also facilitate board wiring by minimizing wiring congestion for this solution also permits in-line wiring. The following chart is a listing of the DIMM locations of a few of these contacts.

NOMINAL CONTACT or SIDE of DISTANCE FROM DIRECTION SIGNAL PIN# DIMM KEY FROM KEY CS0 86 FRONT 11.495 mm RIGHT CS0 224 BACK 11.495 mm LEFT CS1 91 FRONT 16.495 mm RIGHT CS1 229 BACK 16.495 mm LEFT CKE0 65 FRONT 13.505 mm LEFT CKE0 203 BACK 13.505 mm RIGHT CKE1 62 FRONT 16.505 mm LEFT CKE1 200 BACK 16.505 mm RIGHT RAS 222 BACK  9.495 mm LEFT CAS 87 FRONT 12.495 mm RIGHT WE 84 FRONT  9.495 mm RIGHT CK0 77 FRONT  2.495 mm RIGHT CK0 215 BACK  2.495 mm LEFT CK0B 78 FRONT  3.495 mm RIGHT CK0B 216 BACK  3.495 mm LEFT

The ECC function adds a single clock pulse delay (at planned operating frequencies) to the DIMM register performance, which may be of concern to some performance-optimized applications. As such, two additional modes are included on the module that permit the system user to tradeoff performance and reliability. In Parity Mode, the memory interface chip or controller would generate a single parity bit in conjunction with providing the full address and command field to the module. The module would re-drive the address and command bits, to the DRAMs, in the next cycle—rather than adding the additional cycle required in ECC mode. Any error on the address and command bus would be reported to the system at a later time, and the potential for recovery from the fail would be small hence this option is undesirable for many applications. The last mode would be to simply operate the memory in a mode with no parity bits and no ECC bits, with neither the added delay due to ECC nor any means to detect a fault on the address/command bus as per the prior art convention now used for these modules.

FIG. 5 is a block diagram of the SEC/DED ECC circuit of FIG. 4B. The twenty two data inputs 32 a through 32 n via the twenty two latches 72 a through 72 n and lines 82 a through 82 n are fed both to a check bit generator circuit 230 and a first input of a parity generator/checker circuit 231. The parity generator/checker circuit 231 further has a second input coupled to the parity in signal source 31 via primary latch 71 and output line 81 and depending on the state of the parity input signal on input 31 sends a parity error signal (PERR) on output line 111 to the error logic circuit 100.

Meanwhile the check bit generator circuit 230 is transferring the twenty two inputted data signals to a first input of a syndrome bit generator 232 whose second input is coupled to the check bit inputs 30 a through 30 e through the lines 80 a through 80 e coming from the primary latches 70 a through 70 e.

The Syndrome bit generator 232 then transfers the twenty two data signals to a first input of a syndrome bit decoder and the six check bits to the error generator 235 which determines if there are either correctable or uncorrectable errors in the received data and provides the appropriate correctable error or uncorrectable error signal to the error logic circuit 100 via either line 109 or 110. The syndrome bit decoder now decodes the twenty two data bits and transfers them to the data correction circuit 234. In the correction circuit the syndrome bits are selectively X ored with the data inputs consistent with the H-matrix, shown in FIG. 6, with any single bit errors in the data field inverted to correct the error.

The Error Logic block 100 consists of 3 major elements (not shown) which are an error counter, a status register block that contains a plurality of status registers, and an IIC logic block all of which are interconnected through common logic circuits. All of these blocks as well as the interconnecting logic circuits are common and readily available circuits known to those skilled in the art.

More specifically, the error counter is a 16-bit counter that increments as it receives errors inputs (CE, UE or Parity) from the SEC/DED ECC 90. This error counter continues to count errors (until it reaches its full count) even while the status registers are being read out on the IIC bus.

The status register block includes, in the present case, nine eight bit register sets (0-8) which contain information on the data input (DO-21) signals, the check bit signals (C0-5 and Parity In) signals received from the memory controller 19 as well as signals from the memory module 20 (FCC/Parity Mode, SAO-2), the error count, and the syndrome bits (S0-5) which are calculated by the SEC/DED ECC 90.

The IIC Logic block consists of the necessary logic to support the ““IIC Bus Specifications Version 2.1 January 2000 Standard”. In this case the register is an IIC slave where the register is addressed by the DIMM address input range sources (SA0, SA1, SA2) 78 a, 78 b and 78 c and responds to several IIC bus commands—reset, read from the nine (9) Status Registers and the test mode.

The miscellaneous logic circuits interconnecting the above described error counter, status register block and IIC logic block include logic circuits designed to reset the error counters and the nine (9) status registers from either the external reset signal (/RST) source 37 or an internal power-on reset, to load the contents of the nine status registers and logic (including a set of shadow registers) that the IIC logic will send out onto the IIC bus when a IIC bus read occurs, along with some control logic to drive the correctable error (CE) and uncorrectable error (UE) lines out if such an error occurs.

The error bus that comprises nine (9) registers that can be read and reset via an IIC bus) permits the device to be interrogated for additional error information, such as the error type (correctable, uncorrectable or parity error), error count and the memory card location (via the SA0-2 address pins, also shared by the separate SPD EPROM). Other information is also available for diagnostics such as the signals received by the register (address/command, control signals, check bits, parity bit) associated with a CS is active low and the syndrome bits so that they can be decoded to determine, in the case of a failure, which of the 28 input signals (22 ‘CS-gated plus 6 check bits) failed. These registers will contain information about the first fail, and the error counter will continue to increment until it is reset or reaches the full count (64K). All registers can be reset by writing the Reset Error Bus command on the IIC bus.

The Byte 0: Status Register is the general status bit register that can be read to determine the type of error, the mode and the address of the DIMM (same as the DIMM SPD address).

Byte 0: Status Register Bit 7 Bit 6 Bit 5 Bit 4 Bit 3 Bit 2 Bit 1 Bit 0 RFU DIMM DIMM DIMM Mode Parity ECC error ECC error 0 Address Address Address 1=ECC Error 1=UE 1=CE SA2 SA1 SA0 0-Pty 1=PERR Bytes 1 and 2: Error Counter

The 16 bit error counter will count up to 64K errors (FFFF hex) based on any error (CE, UE or Parity Error). Byte 1 is the LSB and byte 2 is the MSB of the error counter. Once the 16-bit counter has counted up to all ones, it will stay all 1s until the error bus is reset. The error counter register will not increment during a IIC read operation but will continue to count errors if they occur.

Bit 7 Bit 6 Bit 5 Bit 4 Bit 3 Bit 2 Bit 1 Bit 0 Byte 1 (LSB) E7 E6 E5 E4 E3 E2 E1 E0 Byte 2 (MSB) E15 E14 E13 E12 E11 E1O E9 E8 Bytes 3-7: Data Registers

Bytes 3-7 show the polarity of all 28 signals of the addresses and commands plus the check bits and parity bit that were received at the time of the first fail.

Bit 7 Bit 6 Bit 5 Bit 4 Bit 3 Bit 2 Bit 1 Bit 0 Byte 3: Data Register A (DO-7) D7 D6 D5 D4 D3 D2 D1 D0 Byte 4: Data Register B (D8-15) D15 D14 D13 D12 D11 D10 D9 D8

Bit 7 Bit 6 Bit 5 Bit 4 Bit 3 Bit 2 Bit 1 Bit 0 Byte 5: Data Register C (D16-21, CSO-1) CS1 CS0 D21 D20 D19 D18 D17 D16 Byte 6: Data Register D (CKE0-1, ODT0-1) RFU RFU 0 RFU 0 RFU 0 ODT1 ODT0 CKE1 CKE0 0 Byte 7: Check Bit (CO-5) and Parity Register RFU RFU 0 Check Check Check Check Check Check 0 Bit 5 Bit 4 Bit 3 Bit 2 Bit 1 Bit 0/Pty In Byte 8: Syndrome Register

Byte 8 shows the syndrome bits associated with the first error. These can be decoded to determine which of the 22 ‘CS-gated signals or 6 Check Bits caused the fail. Bytes 3-7 show the polarity of all input signals at the time of the fail.

FIG. 8 shows the timing diagram used with the present invention.

Byte 8: Syndrome Bit (0-5) Register Bit 7 Bit 6 Bit 5 Bit 4 Bit 3 Bit 2 Bit 1 Bit 0 RFU RFU Syndrome Syndrome Syndrome Syndrome Syndrome Syndrome 0 0 Bit 5 Bit 4 Bit 3 Bit 2 Bit 1 Bit 0

All the information necessary for one skilled in the art to design this error logic block 100 is included in the H-Matrix shown in FIG. 6 where D0 through D21 indicate refer to the data bits, C0 through C5 refer to the check bits and S0 through S5 refer to the syndrome bits.

In order to detect if the module installed in the server can properly monitor the address and control bus integrity, correct errors on the address and control bus, report errors and log and counts errors it is necessary that the DIMM error bus be functional and correctly accessed using the industry IIC protocol and the SA 0-1 bits such that the DIMM can provide a byte of data which includes Byte 0 discussed above. This is achieved by echoing back the SA 0-2 bits on bits 4, 5, and 6 of the Byte 0 and having bit 3 (the ECC flag bit) at a “1” or high level. This proves a unique signature. If the match does not occur the module is incapable of monitoring the address and control bus integrity, correcting errors on the address and control bus, reporting errors or logging and counting detected errors

Parity error reporting in the present invention is realized by delivering the parity signal one cycle after the address and command to which it applies, and driving the error line low, i.e., “0” two clock cycles after the address and command bits are driven to the DRAMs from the memory interface chip if an error is detected. After holding the error line low for only 2 clock cycles, the driver will be disabled and the output permitted to return to an undriven state (high impedance) allowing this line to be shared by multiple modules.

The invention also provides a means for and a method for adjusting the propagation delay for signals on the memory module that are not included in the ECC circuitry such that the signals can be selectively re-driven within one or two clock cycles. This results in a significant increase in module operating speed.

Moreover by operating the memory module in parity mode, unused ECC check bit inputs can be held at a low level, i.e., “0” thus ensuring that these inputs are at a known and quiescent state.

Finally the module of the invention may be operated as if it were a conventional non-ECC protected module, by effective removing the secondary registers (post-ECC) from the delay path by setting the /ECC Mode control pin to a high level, i.e. “1”.

In summary, the present invention is an enhanced function 28 bit 1:2 register, intended for use on main memory modules. The register, of the present invention, adds ECC logic to correct single bit errors and permit continuous memory operation independent of the existence of these errors. A parity operating mode is also provided, in conjunction with error reporting circuitry to permit the system to interrogate the device to determine the error condition.

The present invention also provides CS gating of key inputs (/CS0, CS1, CS Gate Enable). As a means to reduce device power, the register's internal latches will only be updated when one or both of the CS inputs are active low (and CS Gate Enable tied high) at the rising edge of clock. The 22 ‘CS-gated signals associated with this function include addresses (addr 0:15, BA 0:2). RAS, CAS, WE—with the remaining signals (CS, CKE, ODT) continuously re-driven at the rising edge of every clock as they are independent of CS. The CS gating function can be disabled by tying CS Gate Enable low enabling all internal latches to be updated on every rising edge of clock.

Programmable delay for un-gated inputs (/Delay CK-ODT) is also provided. For the pins associated with CKE and ODT (DRAM signals), the inputs will be latched and re-driven on each rising edge of CLK (, independent of the state of the chip select (CS). However, since some controllers may be designed with limited flexibility regarding latency for these signals vs CS, Addr, RAS, CAS and WE. a delay block can be selected to re-align the timing relationships which are offset by one clock cycle when the error correction code is enabled.

Also for all inputs gated by CS, the on-chip SEC/DED ECC logic is enabled and the signal received on CHK0/Parity In is received as check bit 0 via a programming pin (/ECC Mode low). This ECC logic will operate across 28 inputs (22 CS-gated inputs and the 6 check bits), and will correct all single bit errors present on the 22 CS-gated inputs./Error (CE) will be driven low for two clocks and errors will be counted and latched in the Error Bus Registers for the 28 inputs. Any double bit error will also be detected (as well as any error that is not correctable), and will be reported on the /Error (UE) error line (driven low for two clocks) and in the Error Bus Registers. Although CS0-1 are not included in the ECC logic, the propagation delay of the CS output signals will track the signals included in the ECC logic (1 additional clock of latency).

In addition to the above ECC mode, the same 22 CS-gated signals can be operated in ‘parity mode (/ECC Mode high), whereby the signal received on CHK0/Parity In is received as parity to the register 1 clock later than the ‘CS-gated inputs. The received parity bit is then compared to the parity calculated across these same inputs by the register parity logic to verify that the information has not been corrupted. The 22 ‘CS-gated signals will be latched and re-driven on the first clock and any error will be reported two clocks later via the /Error (UE) line (driven low for two clocks) and in the Error Bus Registers. No correction of errors will be completed in this mode. The convention of parity is odd parity (odd numbers of 1's across data and parity inputs equals valid parity).

The /RST pin is used to clear all internal latches (including the error registers), and all outputs will be driven low quickly except the error lines which will be driven high.

The error reporting circuitry, of the present invention is included to permit external monitoring of device operation. Two open-drain outputs are available to permit multiple modules to share a common signal pin for reporting an error that occurred during a valid command (/CS=low) cycle (consistent with the re-driven signals). These two outputs are driven low for two clocks to allow the memory controller time to sense the error./Error (CE) indicates that a correctable error occurred and was corrected by the ECC logic./Error (UE) indicates that an uncorrectable error occurred and depending on the mode selected is an uncorrectable ECC error or a parity error. Note that the timing of UE is different in parity mode vs ECC mode.

In addition, the error bus, (the nine registers discussed above that can be read and reset via an IIC bus) is available to permit the device to be interrogated for additional error information, such as the error type (correctable, uncorrectable or parity error), error count and the memory card location (via the SA0-2 address pins, also shared by the separate SPD EPROM). Other information is also available for diagnostics such as the signals received by the register (address/command, control signals. check bits, parity bit) when a CS is active low and the syndrome bits so that they can be decoded to determine which of the 28 input signals (22 ˜CS-gated plus 6 check bits) failed. These registers will contain information about the first fail, and the error counter will continue to increment until it is reset or reaches the full count (64K). All registers can be reset by writing the Reset Error Bus command on the IIC bus.

This completes the description of the preferred embodiment of the invention. Since changes may be made in the above construction without departing from the scope of the invention described herein, it is intended that all the matter contained in the above description or shown in the accompanying drawings shall be interpreted in an illustrative and not in a limiting sense. Thus other alternatives and modifications will now become apparent to those skilled in the art without departing from the spirit and scope of the invention as set forth in the following claims. 

1. A method of operating a server for detecting the status of a DIMM inserted therein to assure the DIMM can monitor the address and control bus integrity, and can correct errors on the address and control bus and report errors and log and count errors consisting of the steps of; accessing said DIMM using an industry standard IIC protocol and address input range sources (SA0, SA1, SA2), activating said DIMM to produce a byte of data which includes the contents of Byte 0, i.e., Bit 7 Bit 6 Bit 5 Bit 4 Bit 3 Bit 2 Bit 1 Bit 0 RFU DIMM DIMM DIMM Mode Parity ECC ECC 0 Address Address Address 1=ECC Error error error SA2 SA1 SA0 0=Pty 1= 1=UE 1=CE PERR

stimulating the DIMM to ensure that the DIMM echoes back the same SA0, SA1, and SA2 address as that sent to the DIMM: and verifying that a high signal level (a “1”) is present on bit
 3. 2. A method of operating a memory system to enable determination of the type of an installed memory module, the method comprising: accessing the memory module using an IIC bus and a standard IIC bus read protocol, the access including a module location address of the memory module location being read in a bus read command; receiving a response to the bus read command, the response including module location address information for the memory module; and comparing the received address information with the sent module location address to determine one or more of the existence and the type of the memory module.
 3. The method of claim 2 wherein the module location address is the same as the module SPD address.
 4. The method of claim 2 wherein the module location address comprises an SA0, an SA1 and an SA2 bit.
 5. The method of claim 2 wherein the response further includes information regarding one or more of functions supported by the module, error information and other information regarding the installed module.
 6. The method of claim 2, wherein the memory module is a dual inline memory module (DIMM).
 7. The method of claim 2, wherein the bus read results in a response from a re-drive device located on the module.
 8. The method of claim 7 wherein the re-drive device is a register that shares the module location address information with an SPD EPROM.
 9. A method of operating a memory system to enable determination of the memory module type that is installed, the method comprising: accessing one or more registers integrated into a re-drive device on the module, the re-drive device further connected to one or more memory devices, the accessing completed using an IIC bus and standard IIC bus read protocol, and the access including the sending of the module location address of the memory module being read by setting one or more module location address bits identifying that module position; receiving a response to the read operation, the response including contents of one or more registers containing status information including one or more of the module address location, an operating mode for the module and error information; and analyzing the received response to determine one or more of a memory module mode, an existence of the module, a type of the module and an error type.
 10. The method of claim 9 wherein the module address location is the same as the module SPD address.
 11. The method of claim 9 wherein the module location address comprises an SA0, an SA1 and an SA2 bit.
 12. The method of claim 9, wherein the memory module is a DIMM having 276 pins.
 13. The method of claim 9 wherein the response analysis includes a determination if the module installed is operable for the intended use.
 14. The method of claim 13 wherein the intended use includes the ability of the module to monitor address and controller bus integrity and correct errors on the address and control bus.
 15. The method of claim 9, wherein the bus read operation results in a response from a re-drive device located on the module.
 16. The method of claim 15 wherein the re-drive device is a register, wherein the register shares the module location address information with an SPD EPROM.
 17. The method of claim 15 wherein the re-drive device includes one or more output drivers having a ratio of at least 2 signal outputs for each input signal. 